EP3396685B1 - Composant composite comprenant un aimant lié en forme d'anneau et son procédé de fabrication - Google Patents

Composant composite comprenant un aimant lié en forme d'anneau et son procédé de fabrication Download PDF

Info

Publication number
EP3396685B1
EP3396685B1 EP18169460.5A EP18169460A EP3396685B1 EP 3396685 B1 EP3396685 B1 EP 3396685B1 EP 18169460 A EP18169460 A EP 18169460A EP 3396685 B1 EP3396685 B1 EP 3396685B1
Authority
EP
European Patent Office
Prior art keywords
particles
rubber
mass
magnetic
compound
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
EP18169460.5A
Other languages
German (de)
English (en)
Other versions
EP3396685A1 (fr
Inventor
Rie Yoshida
Masahiro Abe
Michiya Kume
Kohei Ihara
Shuichi Tada
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nichia Corp
Original Assignee
Nichia Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from JP2018073347A external-priority patent/JP6544456B2/ja
Application filed by Nichia Corp filed Critical Nichia Corp
Priority to EP20164257.6A priority Critical patent/EP3690901B1/fr
Publication of EP3396685A1 publication Critical patent/EP3396685A1/fr
Application granted granted Critical
Publication of EP3396685B1 publication Critical patent/EP3396685B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F1/00Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties
    • H01F1/01Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials
    • H01F1/03Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity
    • H01F1/032Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of hard-magnetic materials
    • H01F1/04Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of hard-magnetic materials metals or alloys
    • H01F1/047Alloys characterised by their composition
    • H01F1/053Alloys characterised by their composition containing rare earth metals
    • H01F1/055Alloys characterised by their composition containing rare earth metals and magnetic transition metals, e.g. SmCo5
    • H01F1/059Alloys characterised by their composition containing rare earth metals and magnetic transition metals, e.g. SmCo5 and Va elements, e.g. Sm2Fe17N2
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F41/00Apparatus or processes specially adapted for manufacturing or assembling magnets, inductances or transformers; Apparatus or processes specially adapted for manufacturing materials characterised by their magnetic properties
    • H01F41/02Apparatus or processes specially adapted for manufacturing or assembling magnets, inductances or transformers; Apparatus or processes specially adapted for manufacturing materials characterised by their magnetic properties for manufacturing cores, coils, or magnets
    • H01F41/0253Apparatus or processes specially adapted for manufacturing or assembling magnets, inductances or transformers; Apparatus or processes specially adapted for manufacturing materials characterised by their magnetic properties for manufacturing cores, coils, or magnets for manufacturing permanent magnets
    • H01F41/0266Moulding; Pressing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29BPREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
    • B29B7/00Mixing; Kneading
    • B29B7/002Methods
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C45/00Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
    • B29C45/0013Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor using fillers dispersed in the moulding material, e.g. metal particles
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08LCOMPOSITIONS OF MACROMOLECULAR COMPOUNDS
    • C08L77/00Compositions of polyamides obtained by reactions forming a carboxylic amide link in the main chain; Compositions of derivatives of such polymers
    • C08L77/02Polyamides derived from omega-amino carboxylic acids or from lactams thereof
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F1/00Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties
    • H01F1/01Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials
    • H01F1/03Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity
    • H01F1/032Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of hard-magnetic materials
    • H01F1/04Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of hard-magnetic materials metals or alloys
    • H01F1/047Alloys characterised by their composition
    • H01F1/053Alloys characterised by their composition containing rare earth metals
    • H01F1/0533Alloys characterised by their composition containing rare earth metals in a bonding agent
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F1/00Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties
    • H01F1/01Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials
    • H01F1/03Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity
    • H01F1/032Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of hard-magnetic materials
    • H01F1/04Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of hard-magnetic materials metals or alloys
    • H01F1/06Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of hard-magnetic materials metals or alloys in the form of particles, e.g. powder
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F1/00Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties
    • H01F1/01Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials
    • H01F1/03Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity
    • H01F1/032Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of hard-magnetic materials
    • H01F1/04Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of hard-magnetic materials metals or alloys
    • H01F1/06Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of hard-magnetic materials metals or alloys in the form of particles, e.g. powder
    • H01F1/08Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of hard-magnetic materials metals or alloys in the form of particles, e.g. powder pressed, sintered, or bound together
    • H01F1/083Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of hard-magnetic materials metals or alloys in the form of particles, e.g. powder pressed, sintered, or bound together in a bonding agent
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F1/00Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties
    • H01F1/01Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials
    • H01F1/03Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity
    • H01F1/032Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of hard-magnetic materials
    • H01F1/10Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of hard-magnetic materials non-metallic substances, e.g. ferrites, e.g. [(Ba,Sr)O(Fe2O3)6] ferrites with hexagonal structure
    • H01F1/11Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of hard-magnetic materials non-metallic substances, e.g. ferrites, e.g. [(Ba,Sr)O(Fe2O3)6] ferrites with hexagonal structure in the form of particles
    • H01F1/113Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of hard-magnetic materials non-metallic substances, e.g. ferrites, e.g. [(Ba,Sr)O(Fe2O3)6] ferrites with hexagonal structure in the form of particles in a bonding agent
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F7/00Magnets
    • H01F7/02Permanent magnets [PM]
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F2998/00Supplementary information concerning processes or compositions relating to powder metallurgy
    • B22F2998/10Processes characterised by the sequence of their steps
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/22Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces for producing castings from a slip
    • B22F3/225Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces for producing castings from a slip by injection molding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
    • B22F7/06Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
    • B22F7/08Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools with one or more parts not made from powder
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C45/00Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
    • B29C45/14Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor incorporating preformed parts or layers, e.g. injection moulding around inserts or for coating articles
    • B29C45/1459Coating annular articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2077/00Use of PA, i.e. polyamides, e.g. polyesteramides or derivatives thereof, as moulding material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/0005Condition, form or state of moulded material or of the material to be shaped containing compounding ingredients
    • B29K2105/0044Stabilisers, e.g. against oxydation, light or heat
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B29K2105/16Fillers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2505/00Use of metals, their alloys or their compounds, as filler
    • B29K2505/08Transition metals
    • B29K2505/12Iron
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2683/00Use of polymers having silicon, with or without sulfur, nitrogen, oxygen or carbon only, in the main chain, for preformed parts, e.g. for inserts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2995/00Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
    • B29K2995/0003Properties of moulding materials, reinforcements, fillers, preformed parts or moulds having particular electrical or magnetic properties, e.g. piezoelectric
    • B29K2995/0008Magnetic or paramagnetic

Definitions

  • the present invention relates to a composite component including a ring-shaped bonded magnet and a method of manufacturing the composite component.
  • Rotors provided with ring-shaped permanent magnets such as described in JP 2016-101062 A are known as driving sources of fuel pumps for automobiles, motorcycles, or the like.
  • a magnet is attached to a rotator that serves as a base made of a metal.
  • a method of attaching the magnet to the rotator a method using adhesive force (e.g. by bonding) or mechanical fitting force (e.g. by shrink fitting or fastening) may be used.
  • adhesive force e.g. by bonding
  • mechanical fitting force e.g. by shrink fitting or fastening
  • a technique of integrally molding a bonded magnet with a metal component is used mainly in view of cost reduction.
  • JP 2016-101062 A describes a composite component in which a ring-shaped permanent magnet has been molded integrally on the outer periphery of an annular metal component by injection-molding a magnetic powder, a thermoplastic resin, and a thermoplastic elastomer on the metal component.
  • JP 2002-78257 A describes that, when a plurality of sintered magnets are bonded to the outer surface of a metal rotor core, the magnetic poles are spaced apart from each other, which allows for reducing thermal stress between the rotor core and the magnets.
  • JP 2016-533148 T describes that a metal rotor core and a magnet are solder-bonded, and a plurality of slit recesses are provided in the surface of the rotor core to reduce thermal stress.
  • JP 2008-172965 A describes that, in forming of an anisotropic bonded magnet surrounding a metal shaft, the positions of the welded part and the part between the magnetic poles, i.e., the magnetic-pole switching part, do not coincide.
  • JP 2006-41116 A describes that a bis-unsaturated fatty acid amide may be mixed into a polyamide, which is a base resin that is most-commonly used for bonded magnets, to improve flexibility so that the resulting molded product can exhibit enhanced thermal shock resistance.
  • JP H06-287445 A describes that a liquid rubber may be mixed into polyamide, which is a base resin, to reduce cracks due to mold shrinkage.
  • JP 2005-72240 A describes that materials having appropriately-selected aspect ratios may be combined to allow avoiding cracks or chips in the molded product.
  • JP 2005-151757 A describes that, when a bonded magnet is formed integrally on the outer periphery of a rotor, a middle layer may be provided between the rotor and the bonded magnet to form a bonded magnet made of a material with a high flexural strain to allow for avoiding cracks due to mold shrinkage or thermal cycles.
  • JP 2016-143827 A describes a composite material including: a soft magnetic powder; a filler that contains a rubber particle and an outer peripheral layer disposed on the surface of the rubber particle and containing an organic material; and a resin part in which the soft magnetic powder and the filler are dispersed.
  • the fillers containing the rubber particle are dispersed in the resin part, which allows for obtaining an effect of reducing propagation of microcrack.
  • the filler needs to be subjected to an additional treatment such as surface treatment in order to be compatible with the resin.
  • a ring-shaped bonded magnet molded integrally with a metal component as in the present invention stress due to difference between the coefficient of linear expansion of the metal component and that of the bonded magnet is applied to the resin due to a thermal shock.
  • a sufficient effect of absorbing such stress is not easily obtained by using the technique in which a rubber is dispersed in a resin in a state where the rubber is compatible with the matrix resin.
  • US 2008/199118 A1 relates to a magnetic encoder to be used for detecting a rotational number of a rotating member and a roller bearing unit having the magnetic encoder.
  • the present invention provides a composite component including a ring-shaped bonded magnet having good thermal shock resistance, and a method of manufacturing the composite component.
  • a composite component includes: a metal component having a substantially cylindrical shape or a substantially annular shape; and a ring-shaped bonded magnet disposed on an outer periphery of the metal component, the ring-shaped bonded magnet containing a thermoplastic resin, magnetic particles, and rubber particles of 0. 7 ⁇ m-1mm, as specified in claim 1.
  • a method of manufacturing the composite component includes: kneading a thermoplastic resin with magnetic particles to obtain a compound; and integrally molding the compound and rubber particles with a metal component having a substantially cylindrical shape or a substantially annular shape, as specified in claim 4.
  • the embodiments of the present invention allow for providing a composite component including a ring-shaped bonded magnet having good thermal shock resistance, and a method of manufacturing the composite component.
  • the amount of the component in the composition refers to the total amount of the multiple substances in the composition, unless otherwise stated.
  • the composite component according to one embodiment of the present invention includes a metal component having a substantially cylindrical shape or a substantially annular shape, and a ring-shaped bonded magnet disposed on the outer periphery of the metal component.
  • the ring-shaped bonded magnet contains a thermoplastic resin, magnetic particles, and rubber particles.
  • the metal component has any appropriate shape as long as it is a substantially cylindrical or substantially annular shape.
  • the substantially cylindrical or substantially annular metal component preferably has an outer diameter of 5 mm or greater and 100 mm or less, and it preferably has a height of 1 mm or greater and 30 mm or less.
  • a metal used for the metal component may be any appropriate metal that can serve as a yoke.
  • the composite component including a ring-shaped bonded magnet may also have any appropriate shape as long as it is a substantially cylindrical or substantially annular shape.
  • the outer diameter of the composite component is preferably 6 mm or greater and 150 mm or less, and the height thereof is preferably 1 mm or greater and 30 mm or less.
  • thermoplastic resin any appropriate material may be used for the thermoplastic resin, and examples thereof include polypropylene, polyethylene, polyvinyl chloride, polyester, polyamide, polycarbonate, polyphenylene sulfide, and acrylic resin.
  • polyamide is preferable, and polyamide 12 is particularly preferable.
  • Polyamide 12 is a crystalline resin having a relatively low melting point and a low water absorption rate, and thus shows good moldability.
  • these thermoplastic resins may be used in combination as appropriate.
  • the ring-shaped bonded magnet further contains a thermoplastic elastomer.
  • a thermoplastic elastomer With a thermoplastic elastomer, initial strength can be improved without impairing fluidity.
  • the thermoplastic elastomer include polystyrene, polyolefin, polyester, polyurethane, and polyamide thermoplastic elastomers. These thermoplastic elastomers may be used in combination as appropriate. Preferred among these, polyamide thermoplastic elastomers having good chemical resistance are preferable.
  • the ring-shaped bonded magnet may further contain an antioxidant such as a phosphorus antioxidant.
  • an antioxidant such as a phosphorus antioxidant.
  • a phosphorus antioxidant changes in strength of the composite component over time can be reduced even under high temperature.
  • examples of the phosphorus antioxidant include tris(2,4-di-tert-butylphenyl)phosphite.
  • magnétique particles examples include ferrite magnetic particles and rare earth magnetic particles such as Nd-Fe-B based magnetic particles, Sm-Co based magnetic particles, and Sm-Fe-N based magnetic particles. Among these, Sm-Fe-N based magnetic particles are preferable. Sm-Fe-N based magnetic particles are typically represented by Sm 2 Fe 17 N 3 . Sm-Fe-N magnetic particles have stronger magnetic force than that of ferrite magnetic particles, and even relatively small quantities of Sm-Fe-N can provide high magnetic force.
  • Sm-Fe-N magnetic particles have a smaller particle size than that of other rare earth magnetic particles such as Nd-Fe-B based magnetic particles and Sm-Co based magnetic particles, and thus are suitable as filler for the matrix resin, and are less likely to rust.
  • Anisotropic magnetic particles or isotropic magnetic particles, or a combination of these may be used for the magnetic particles.
  • anisotropic magnetic particles are preferably used.
  • Sm-Fe-N magnetic particles having anisotropy are preferably used. Because Sm-Fe-N-based magnetic particles have a strong magnetic force, using Sm-Fe-N-based magnetic particles for the magnetic particles allows for obtaining better magnetic properties.
  • the magnetic particles preferably have an average particle size of 10 ⁇ m or less, and the average particle size is more preferably 1 ⁇ m or greater and 5 ⁇ m or less.
  • the average particle size is more preferably 1 ⁇ m or greater and 5 ⁇ m or less.
  • defects such as irregularities and cracks on the surface of a product are less likely to occur, and thus the product has a good appearance.
  • the cost can also be reduced.
  • An average particle size of more than 10 ⁇ m may lead to generation of irregularities and cracks on a surface of the product, resulting in a poor appearance.
  • an average particle size of less than 1 ⁇ m the cost of the magnetic particles increases, and thus is not preferable in view of cost reduction.
  • the rubber particles commercially available rubber particles or rubber particles prepared by cross-linking a rubber material and crushing it may be used.
  • any appropriate material may be used, but in view of thermal shock resistance, a rubber having a heat resistance of 120 °C or higher and a cold resistance of -40 °C or lower may preferably be used.
  • the rubber material include silicone rubber (raw silicone rubber), fluororubber, and ethylene-vinyl acetate rubber, among which silicone rubber is particularly preferable in view of its appropriate flexibility, chemical stability, heat resistance, and cold resistance.
  • the rubber particles are rubber magnet particles containing magnetic particles (see Fig. 2 ).
  • magnetic particles as described above may be used.
  • the amount of the magnetic particles in the rubber magnet particles is preferably 50% or greater and 99% or less by mass, and is more preferably 80% or greater and 98% or less by mass, to obtain high magnetic properties.
  • the average particle size of the rubber particles is determined as the particle size corresponding to the 50th percentile from the smallest particle size in a cumulative particle size distribution by volume determined under dry conditions using a laser diffraction particle size analyzer.
  • the average particle size of the rubber particles is greater than 0.7 ⁇ m and less than 1 mm, and in view of thermal shock resistance, it is preferably 2 ⁇ m or greater and 900 ⁇ m or less, and in view of fluidity during molding, it is particularly preferably 11 ⁇ m or greater but 500 ⁇ m or less.
  • the average particle size of the rubber particle is preferably greater than 0.7 ⁇ m and less than 1 mm, more preferably 50 ⁇ m or greater and 900 ⁇ m or less, and in view of fluidity during molding, it is particularly preferably 100 ⁇ m or greater and 800 ⁇ m or less.
  • the amount of the magnetic particles in the ring-shaped bonded magnet is preferably 80% by mass or greater and 95 % by mass or less, more preferably 90% by mass or greater and less than 95% by mass, to obtain high magnetic properties.
  • the amount of the thermoplastic resin in the ring-shaped bonded magnet is preferably 3% by mass or greater and 20% by mass or less, more preferably 5% by mass or greater and 15% by mass or less, to ensure fluidity.
  • the amount of the thermoplastic elastomer in the ring-shaped bonded magnet is preferably such that the ratio by mass of the thermoplastic resin to the thermoplastic elastomer is in a range of 90:10 to 50:50, and more preferably in a range of 90:10 to 70:30 to obtain shock resistance.
  • the amount of the phosphorus antioxidant in the ring-shaped bonded magnet is preferably 0.1% by mass or greater and 2% by mass or less.
  • the amount of the rubber particles in the ring-shaped bonded magnet is preferably 0.3% by mass or greater and 10% by mass or less, more preferably 0.5% by mass or greater and 5.5% by mass or less, in view of thermal shock resistance. In the case where the rubber particles contain no magnetic material, the amount of the rubber particles is further preferably 0.3% by mass or greater and 1.0% by mass or less. In the case where the rubber particles contain rubber magnet particles containing a magnetic material, the amount of the rubber particles is further preferably 0.3% by mass or greater and 10% by mass or less.
  • the method of manufacturing the composite component according to the present invention includes kneading a thermoplastic resin and magnetic particles to obtain a compound, and integrally molding the compound and rubber particles with a substantially cylindrical or substantially annular metal component.
  • a compound containing a thermoplastic resin and magnetic particles is provided separately from rubber particles. If rubber particles are kneaded with a thermoplastic resin and magnetic particles to prepare a compound, the rubber particles are exposed to heat both in the preparation of the compound and in the integral molding, which may lead to decrease in elasticity or strength of the rubber particles. Moreover, the metering torque during the molding will be increased, so that molding temperature is required to be increased. The increase in molding temperature can cause deterioration of the thermoplastic resin, which may result in reduction in thermal shock resistance. In contrast, in the present embodiment, the rubber particles are exposed to heat only at the time of integral molding, the properties of the rubber particles are less likely to deteriorate. Thus, the composite component to be obtained can maintain the elasticity and strength of the rubber particles.
  • the compound in the step of kneading a thermoplastic resin with magnetic particles to obtain a compound, the compound can be obtained by sufficiently kneading a thermoplastic resin and magnetic particles, feeding the kneaded mixture into a kneading machine such as a single-screw or twin-screw kneading machine, cooling, and then cutting into an appropriate size.
  • a kneading machine such as a single-screw or twin-screw kneading machine, cooling, and then cutting into an appropriate size.
  • the thermoplastic resin and the magnetic particles are as described above.
  • thermoplastic elastomer and/or an antioxidant such as a phosphorus antioxidant may be simultaneously kneaded with the thermoplastic resin and magnetic particles.
  • the amount of the magnetic particles in the compound is preferably 80% by mass or greater and 95% by mass or less, and is more preferably 90% by mass or greater and 95% by mass or less to obtain high magnetic properties.
  • the amount of the thermoplastic resin in the compound is preferably 3% by mass or greater and 20% by mass or less, and is more preferably 5% by mass or greater and 15% by mass or less to ensure fluidity.
  • the ratio by mass of the thermoplastic resin to the thermoplastic elastomer is preferably in a range of 90:10 to 50:50, and more preferably in a range of 90:10 to 70:30 in view of shock resistance.
  • the amount of the phosphorus antioxidant in the compound is preferably 0.1% by mass or greater and 2% by mass or less.
  • the rubber particles may be prepared as follows: a rubber material and a vulcanizing agent and a crosslinking agent that are appropriate for the rubber material are kneaded in a kneading machine such as a mixing roll, kneader, or Banbury mixer, and the kneaded mixture is fed into an extruder to obtain a string-like molding, which is then optionally heat-cured and cooled, followed by crushing into the desired size, so that rubber particles can be obtained.
  • a kneading machine such as a mixing roll, kneader, or Banbury mixer
  • the rubber particles are rubber magnet particles containing magnetic particles.
  • a kneading machine such as a mixing roll, kneader, or Banbury mixer
  • the kneaded mixture is fed into an extruder to obtain a string-like molding, which is then optionally heat-cured and cooled, followed by crushing into the desired size, so that rubber magnet particles can be obtained.
  • the magnetic particles and the rubber material are as described above.
  • the expression "at least some of the rubber particles are rubber magnet particles containing magnetic particles” includes both the case where rubber magnet particles and rubber particles that do not contain a magnetic material are mixed, and the case where all of the rubber particles contain magnet particles.
  • a substantially cylindrical or substantially annular metal component is placed in a mold of an injection molding machine, the compound and rubber particles are fed into the injection molding machine, and then integral injection molding is performed.
  • the rubber particles may be contained at any appropriate ratio by mass with respect to the compound, but the amount of the rubber particles is preferably 0.3 parts by mass or greater and 10 parts by mass or less, more preferably 0.5 parts by mass or greater and 5.5 parts by mass or less, per 100 parts by mass of the compound. An amount of lower than 0.3 parts by mass tends to lead to insufficient thermal shock resistance. An amount of higher than 10 parts by mass tends to lead to reduction in magnetic flux density. In the case where the rubber particles contain no magnetic particles, the amount of the rubber particles per 100 parts by mass of the compound is further preferably 0.3 parts by mass or greater and 1.0 parts by mass or less. In the case where the rubber particles are rubber magnet particles containing magnetic particles, the amount of the rubber particles per 100 parts by mass of the compound is further preferably 0.3 parts by mass or greater and 10 parts by mass or less.
  • the composite component according to certain embodiments of the present invention can be used in rotors including ring-shaped permanent magnets and in other driving sources of fuel pumps for vehicles such as automobiles and motorcycles.
  • the average particle size was determined as the particle size corresponding to the 50th percentile from the smallest particle size in a cumulative particle size distribution by volume determined using a laser diffraction particle size analyzer (HELOS & RODOS from Japan Laser Corporation).
  • Magnetic particles anisotropic Sm-Fe-N based magnetic material (average particle size: 3 ⁇ m)
  • Thermoplastic resin polyamide 12
  • the Sm-Fe-N magnetic material was surface-treated with ethyl silicate and a silane coupling agent.
  • the surface-treated Sm-Fe-N based magnetic material (91% by mass) and polyamide 12 (9% by mass) were mixed using a mixer.
  • the mixed powder was kneaded at 220 °C using a twin-screw kneading machine, cooled, and then cut into an appropriate size to obtain a pellet-shaped compound.
  • the compound (100 parts by mass) and the rubber particles A (0.5 parts by mass) were fed into an injection molding machine.
  • An annular metal component ( ⁇ 14 mm (outer diameter) ⁇ 20 mm (height)) was inserted into the mold, and the compound and the rubber particles were then injection-molded into a mold cavity surrounding the outer periphery of the metal component so as to be integrated with the metal component, so that a ring-shaped bonded magnet was formed on the outer periphery of the metal component.
  • the outer diameter of this composite component was ⁇ 21 mm.
  • the injection molding was carried out while applying a magnetic field along the radial direction of the ring-shaped bonded magnet that had been formed.
  • a composite component was prepared as in Example 1, except that the rubber particles B were used instead of the rubber particles A .
  • a composite component was prepared as in Example 1, except that the rubber particles C were used instead of the rubber particles A .
  • a composite component was prepared as in Example 1, except that the rubber particles D were used instead of the rubber particles A.
  • a composite component was prepared as in Example 1, except that no rubber particles were used.
  • a cylindrical bonded magnet having a diameter of ⁇ 10 mm and a height of 7 mm was produced using the compound and rubber particles used in each of the examples and comparative example.
  • the magnetic flux density Br was measured using a BH curve tracer (Riken Denshi Co., Ltd).
  • the magnetic flux density Br values were compared to Comparative Example 1, which was taken as 100. The results are shown in Table 1.
  • Example 1 Example 2 Example 3 Example 4 Comparative Example 1 (A) Compound Magnetic powder Sm 2 Fe 17 N 3 Resin PA 12 (B) Rubber particles Rubber Silicone rubber Silicone rubber Silicone rubber Silicone rubber - Size 2 ⁇ m 4.5 ⁇ m 11 ⁇ m 0.7 ⁇ m - Ratio (A)/(B) (w/w) 100/0.5 100/0.5 100/0.5 100/0.5 - Timing to add (B) to (A) Injection molding Injection molding Injection molding - Thermal shock resistance Number of cracked samples 0/10 0/10 0/10 3/10 10/10 Magnetic flux density Br (%) 98 98 97 95 100
  • Table 1 shows that the composite components of Examples 1 to 4 containing rubber particles exhibited improved thermal shock resistance as compared with Comparative Example 1, while preventing decrease in magnetic flux density Br.
  • a compound was prepared as in Example 1. 0.1% by mass of an addition-type vulcanizing agent, 0.4% by mass of a crosslinking agent, and 77.5% by mass of a surface-treated Sm-Fe-N magnetic material were added to 22% by mass of a raw silicone rubber (cold resistance: -120°C, heat resistance: 280°C), and they were uniformly mixed in an extruder. The mixture was then molded into a string-like shape having a diameter of approximately 2 mm or greater and 4 mm or less using the extruder, and then heat-treated at 150 °C for two hours to obtain a silicone rubber magnet. Subsequently, the rubber magnet was crushed in liquid nitrogen to obtain rubber magnet particles having an average particle size of 150 ⁇ m. Then, a composite component was obtained in a manner as in Example 1, except that the compound and the rubber particles were fed into the injection molding machine at a ratio of 5.0 parts by mass of the rubber magnet particles to 100 parts by mass of the compound.
  • a composite component was obtained in a manner as in Example 5, except that rubber magnet particles having an average particle size of 300 ⁇ m were obtained.
  • a composite component was obtained in a manner as in Example 5, except that rubber magnet particles having an average particle size of 500 ⁇ m were obtained.
  • a composite component was obtained in a manner as in Example 5, except that rubber magnet particles having an average particle size of 1 mm were obtained.
  • Rubber magnet particles were obtained in a manner as in Example 5.
  • a compound was obtained as in Example 1, except that 91% by mass of the Sm-Fe-N magnetic material surface-treated in a manner as in Example 1, 9% by mass of polyamide 12, and the obtained rubber magnet particles having an average particle size of 150 ⁇ m in an amount equivalent to the amount added in Example 5 were mixed using a mixer, and the mixed powder was kneaded in a twin-screw kneading machine at 240 °C.
  • the compound was injection molded as in Example 1 to obtain a composite component.
  • Table 2 shows that the composite components of Examples 5 to 8 containing rubber magnet particles exhibited improved thermal shock resistance as compared with Comparative Example 1 in Table 1, while maintaining the magnetic flux density Br. Moreover, comparison between Example 5 and Comparative Example 2 using the same rubber magnet shows that Example 5 had an improved thermal shock resistance.
  • Comparative Example 2 rubber magnet particles were added to the compound at the time of kneading of the compound, which would lead to increase in metering torque during the injection molding. Accordingly, the molding temperature needed to be increased. Thus, it is considered that the high temperature deteriorated the thermoplastic resin, resulting in reduction in thermal shock resistance. Further, the increase in pressure by about 20% during the injection molding was considered to be due to the increase in hardness of the rubber, which was caused by secondary curing of the silicone rubber during the kneading of the compound and the rubber magnet particles.
  • the Sm-Fe-N magnetic material was surface-treated with ethyl silicate and a silane coupling agent. 91% by mass of the surface-treated Sm-Fe-N magnetic material, 7% by mass of polyamide 12, and 2% by mass of a polyamide elastomer were mixed using a mixer to obtain a mixed powder. The mixed powder was kneaded at 220 °C in a twin-screw kneading machine, cooled, and then cut into an appropriate size to obtain a pellet-shaped compound. The obtained compound and rubber particles as in Example 1 were injection-molded in a manner as in Example 1 to obtain a composite component.
  • Example 9 The compound obtained in Example 9 and rubber particles as in Example 2 were injection-molded in a manner as in Example 1 to obtain a composite component.
  • Example 9 The compound obtained in Example 9 and rubber particles as in Example 3 were injection molded in a manner as in Example 1 to obtain a composite component.
  • Example 9 The compound obtained in Example 9 was injection-molded as in Example 1 to obtain a composite component.
  • Example 9 Example 10
  • Comparative Example 3 (A) Compound Magnetic powder Sm 2 Fe 17 N 3 Resin
  • PA 12 PA elastomer
  • B Rubber particles Rubber Silicone rubber Size 2 ⁇ m 4.5 ⁇ m 11 ⁇ m - Ratio (A)/(B) (w/w) 100/0.5 100/0.5 100/0.5 - Timing to add (B) to (A) Injection molding Injection molding Injection molding - Thermal shock resistance Number of cracked samples 0/10 0/10 0/10 1/10 Magnetic flux density Br (%) 91 92 90 92
  • Table 3 shows that the composite components of Examples 9 to 11 containing rubber particles exhibited improved thermal shock resistance as compared with Comparative Example 3, while preventing decrease in magnetic flux density.
  • Example 9 The compound obtained in Example 9 and rubber magnet particles as in Example 5 were injection-molded in a manner as in Example 1 to obtain a composite component.
  • Example 9 The compound obtained in Example 9 and rubber magnet particles as in Example 6 were injection-molded in a manner as in Example 1 to obtain a composite component.
  • Example 9 The compound obtained in Example 9 and rubber magnet particles as in Example 7 were injection-molded in a manner as in Example 1 to obtain a composite component.
  • Example 12 Example 13
  • Example 14 (A) Compound Magnetic powder Sm 2 Fe 17 N 3 Resin PA 12
  • PA elastomer (B) Rubber magnet particles Magnetic powder Sm 2 Fe 17 N 3 Rubber Silicone rubber Size 150 ⁇ m 300 ⁇ m 500 ⁇ m Ratio (A)/(B) (w/w) 100/5 100/5 100/5 Timing to add (B) to (A) Injection molding Injection molding Injection molding Thermal shock resistance Number of cracked samples 0/10 0/10 0/10 Magnetic flux density Br (%) 94 94 95
  • Table 4 shows that the composite components of Examples 12 to 14, which contain rubber magnet particles, exhibited further improved thermal shock resistance while maintaining the magnetic flux density.
  • Fig. 1 shows a photograph of a cross-section of the bonded magnet prepared in Example 7 taken with a light microscope. As shown in Fig. 1 , in the bonded magnet containing a magnetic powder, a thermoplastic resin, and rubber magnet particles, a rubber magnet 6 was present as a particle.
  • the composite components including a ring-shaped bonded magnet according to certain embodiments of the present invention may be used to provide rotating machines (e.g. motors) having good thermal shock resistance. Such rotating machines therefore can be suitably used as driving sources of fuel pumps for vehicles such as automobiles and motorcycles.
  • rotating machines e.g. motors
  • Such rotating machines therefore can be suitably used as driving sources of fuel pumps for vehicles such as automobiles and motorcycles.

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Manufacturing & Machinery (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Inorganic Chemistry (AREA)
  • Mechanical Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Dispersion Chemistry (AREA)
  • Electromagnetism (AREA)
  • Health & Medical Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Medicinal Chemistry (AREA)
  • Polymers & Plastics (AREA)
  • Organic Chemistry (AREA)
  • Hard Magnetic Materials (AREA)
  • Manufacturing Cores, Coils, And Magnets (AREA)
  • Powder Metallurgy (AREA)

Claims (5)

  1. Composant composite comprenant :
    un composant métallique (1) ayant une forme essentiellement cylindrique ou une forme essentiellement annulaire ; et
    un aimant collé de forme annulaire (2) disposé sur une périphérie extérieure du composant métallique (1),
    l'aimant collé de forme annulaire (2) comprenant une résine thermoplastique (4), des particules magnétiques (3) et des particules de caoutchouc (6),
    caractérisé en ce que la granulométrie moyenne des particules de caoutchouc (6) est supérieure à 0,7 µm et inférieure à 1 mm.
  2. Composant composite selon la revendication 1, dans lequel au moins certaines des particules de caoutchouc (6) sont des particules de caoutchouc aimanté (6) contenant des particules magnétiques.
  3. Composant composite selon la revendication 1 ou 2, dans lequel chacune des particules de caoutchouc (6) comprend du caoutchouc de silicone (5).
  4. Procédé de fabrication d'un composant composite selon les revendications 1 à 3, le procédé comprenant :
    le malaxage d'une résine thermoplastique (4) avec des particules magnétiques (3) pour que soit obtenu un composé ; et
    le moulage intégral du composé et des particules de caoutchouc (6) avec un composant métallique (1) ayant une forme essentiellement cylindrique ou une forme essentiellement annulaire.
  5. Procédé selon la revendication 4,
    dans lequel les particules de caoutchouc (6) sont ajoutées en une quantité de 0,3 partie en masse ou plus et 10 parties en masse ou moins pour 100 parties en masse du composé.
EP18169460.5A 2017-04-28 2018-04-26 Composant composite comprenant un aimant lié en forme d'anneau et son procédé de fabrication Active EP3396685B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP20164257.6A EP3690901B1 (fr) 2017-04-28 2018-04-26 Composant composite comprenant un aimant lié en forme d'anneau et son procédé de fabrication

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP2017089571 2017-04-28
JP2018073347A JP6544456B2 (ja) 2017-04-28 2018-04-05 環状ボンド磁石を備える複合部材およびその製造方法

Related Child Applications (2)

Application Number Title Priority Date Filing Date
EP20164257.6A Division EP3690901B1 (fr) 2017-04-28 2018-04-26 Composant composite comprenant un aimant lié en forme d'anneau et son procédé de fabrication
EP20164257.6A Division-Into EP3690901B1 (fr) 2017-04-28 2018-04-26 Composant composite comprenant un aimant lié en forme d'anneau et son procédé de fabrication

Publications (2)

Publication Number Publication Date
EP3396685A1 EP3396685A1 (fr) 2018-10-31
EP3396685B1 true EP3396685B1 (fr) 2020-06-03

Family

ID=62091691

Family Applications (2)

Application Number Title Priority Date Filing Date
EP18169460.5A Active EP3396685B1 (fr) 2017-04-28 2018-04-26 Composant composite comprenant un aimant lié en forme d'anneau et son procédé de fabrication
EP20164257.6A Active EP3690901B1 (fr) 2017-04-28 2018-04-26 Composant composite comprenant un aimant lié en forme d'anneau et son procédé de fabrication

Family Applications After (1)

Application Number Title Priority Date Filing Date
EP20164257.6A Active EP3690901B1 (fr) 2017-04-28 2018-04-26 Composant composite comprenant un aimant lié en forme d'anneau et son procédé de fabrication

Country Status (3)

Country Link
US (2) US11056255B2 (fr)
EP (2) EP3396685B1 (fr)
CN (1) CN108806913B (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3859941A1 (fr) * 2020-01-30 2021-08-04 Max Baermann GmbH Composant aimant pourvu de composé d'aimant élastique
US20220103036A1 (en) * 2020-09-29 2022-03-31 Nichia Corporation Yoke for rotor of axial gap motor

Family Cites Families (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS57187910A (en) * 1981-05-14 1982-11-18 Daido Steel Co Ltd Ferromagnetic formed body
US4670726A (en) * 1984-12-20 1987-06-02 Hitachi Metals, Ltd. Convergence device for electron beams in color picture tube
JP2940572B2 (ja) * 1991-08-09 1999-08-25 株式会社三協精機製作所 希土類ボンド磁石
JPH06287445A (ja) 1993-03-30 1994-10-11 Toda Kogyo Corp ポリアミド系プラスチック磁石用材料
JP2000323322A (ja) 1999-03-05 2000-11-24 Kanegafuchi Chem Ind Co Ltd マグネットローラ
JP2001068316A (ja) * 1999-08-24 2001-03-16 Tdk Corp 樹脂結合型希土類磁石
JP2002078257A (ja) 2000-08-24 2002-03-15 Mitsubishi Electric Corp モーター及びそのローター
JP4548572B2 (ja) 2003-08-25 2010-09-22 戸田工業株式会社 ボンド磁石組成物および該組成物からなる成形品
JP2005151757A (ja) 2003-11-19 2005-06-09 Mate Co Ltd ローター及びローターの製造方法
JP2005237047A (ja) 2004-02-17 2005-09-02 Yaskawa Electric Corp ボンド磁石一体成形ロータ
JP2005241289A (ja) 2004-02-24 2005-09-08 Nsk Ltd 磁気エンコーダ及び当該磁気エンコーダを備えた転がり軸受
JP2006041116A (ja) 2004-07-26 2006-02-09 Toshiba Components Co Ltd 複合トランジスタモジュール
WO2006121052A1 (fr) * 2005-05-10 2006-11-16 Nsk Ltd. Codeur magnetique et unite de palier a roulement comprenant un codeur magnetique
CN101175974B (zh) * 2005-05-10 2011-03-30 日本精工株式会社 磁编码器和具有磁编码器的滚柱轴承
JP4639953B2 (ja) 2005-05-24 2011-02-23 日本精工株式会社 磁気エンコーダ及び前記磁気エンコーダを備える転がり軸受ユニット
US20070172164A1 (en) * 2006-01-20 2007-07-26 Jtekt Corporation Rolling bearing system for vehicles
CN100437841C (zh) * 2006-09-19 2008-11-26 北京大学 各向异性稀土永磁材料及其磁粉和磁体的制造方法
JP2008172965A (ja) 2007-01-15 2008-07-24 Matsushita Electric Ind Co Ltd 永久磁石回転子及びモータ並びに電気機器
JP2008309717A (ja) 2007-06-15 2008-12-25 Nsk Ltd 磁気エンコーダ、及び該磁気エンコーダを備えた転がり軸受ユニット
CN202473522U (zh) * 2012-03-07 2012-10-03 天通控股股份有限公司 一种功率电感用复合软磁磁心
CN102610370A (zh) * 2012-03-07 2012-07-25 天通控股股份有限公司 一种抗电磁干扰用复合软磁磁心
JP2013244653A (ja) 2012-05-25 2013-12-09 Ube Industries Ltd 熱可塑性樹脂組成物と金属の複合体
CN102723165B (zh) * 2012-06-05 2016-05-11 义乌市磁莱福磁铁有限公司 一种粘结钕铁硼强磁铁及其制备方法
DE102013220562A1 (de) 2013-10-11 2015-04-16 Robert Bosch Gmbh Baugruppe für eine elektrische Maschine, Verfahren zur Herstellung einer Baugruppe und elektrische Maschine mit einer Baugruppe
JP6429604B2 (ja) 2014-11-26 2018-11-28 ミネベアミツミ株式会社 熱衝撃に強いボンド磁石を搭載したインナーロータ型モータ
JP6403093B2 (ja) 2015-02-04 2018-10-10 住友電気工業株式会社 複合材料、磁気部品用の磁性コア、リアクトル、コンバータ、及び電力変換装置
CN105023683A (zh) 2015-07-27 2015-11-04 合肥凯士新材料贸易有限公司 一种具有高韧性的钐钴永磁体

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None *

Also Published As

Publication number Publication date
US11056255B2 (en) 2021-07-06
EP3690901A1 (fr) 2020-08-05
CN108806913B (zh) 2021-11-23
EP3690901B1 (fr) 2021-10-27
US20180315526A1 (en) 2018-11-01
US11646154B2 (en) 2023-05-09
CN108806913A (zh) 2018-11-13
EP3396685A1 (fr) 2018-10-31
US20210287832A1 (en) 2021-09-16

Similar Documents

Publication Publication Date Title
US11646154B2 (en) Composite component comprising ring-shaped bonded magnet and method of manufacturing the same
CN105839006B (zh) R-t-b系稀土磁铁粉末的制造方法、r-t-b系稀土磁铁粉末和粘结磁铁
DE112011100698T5 (de) Verbesserte Magnetrotorvorrichtung mit verbesserter physikalischer Festigkeit
EP3780351A1 (fr) Moteur électrique et élément de champ
WO2021014837A1 (fr) Additif pour aimant lié et procédé de fabrication de composé pour aimant lié
CN1199204C (zh) 高耐气候性磁铁粉的制造方法及得到的产品
JP2006344768A (ja) ボンド磁石用組成物、その製造方法、およびそれを用いたロータ磁石並びにブラシレスモータ
US5288447A (en) Method of making permanent magnet rotors
JP2017055509A (ja) 電動機要素の製造方法、電動機要素、電動機、装置
US20220103036A1 (en) Yoke for rotor of axial gap motor
EP3174073B1 (fr) Composition pour aimants liés, aimant lié et composant moulé d'un seul bloc
JP7189445B2 (ja) 環状ボンド磁石を備える複合部材およびその製造方法
US20240013961A1 (en) Composite component and method for producing same
US20220362843A1 (en) Methods of producing bonded magnet and compound for bonded magnets
US6737451B1 (en) Thermally stable, high temperature, samarium cobalt molding compound
US20230128480A1 (en) Compression-bonded magnet, manufacturing method therefor, and field magnetic element
JPS5816509A (ja) 強磁性成形体
JP3735915B2 (ja) 樹脂結合型磁石用組成物及びそれを用いた樹脂結合型磁石
JPH06287445A (ja) ポリアミド系プラスチック磁石用材料
JP2017085837A (ja) 電動機要素、電動機要素の製造方法、電動機、装置
US20160027567A1 (en) Manufacturing Method for Bonded Magnet and Motor Using the Magnet
JP4502292B2 (ja) 合成樹脂磁石組成物およびそれを用いた合成樹脂磁石成形物
JP2003041116A (ja) ポリアミド系プラスチック磁性材料、およびそれから作製された磁石
JPH0618128B2 (ja) マグネットロールの製造方法
JP2004221497A (ja) 内部に金属部分を有するポリアミド系プラスチック磁石

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION HAS BEEN PUBLISHED

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20190429

RBV Designated contracting states (corrected)

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: DE

Ref legal event code: R079

Ref document number: 602018004998

Country of ref document: DE

Free format text: PREVIOUS MAIN CLASS: H01F0001080000

Ipc: H01F0041020000

RIC1 Information provided on ipc code assigned before grant

Ipc: B22F 7/08 20060101ALN20191030BHEP

Ipc: H01F 41/02 20060101AFI20191030BHEP

Ipc: B22F 3/22 20060101ALN20191030BHEP

Ipc: H01F 1/08 20060101ALI20191030BHEP

Ipc: B22F 8/00 20060101ALN20191030BHEP

Ipc: H01F 1/113 20060101ALI20191030BHEP

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

RIC1 Information provided on ipc code assigned before grant

Ipc: H01F 1/113 20060101ALI20191128BHEP

Ipc: H01F 41/02 20060101AFI20191128BHEP

Ipc: B22F 8/00 20060101ALN20191128BHEP

Ipc: H01F 1/08 20060101ALI20191128BHEP

Ipc: B22F 7/08 20060101ALN20191128BHEP

Ipc: B22F 3/22 20060101ALN20191128BHEP

RIC1 Information provided on ipc code assigned before grant

Ipc: H01F 1/08 20060101ALI20191202BHEP

Ipc: B22F 3/22 20060101ALN20191202BHEP

Ipc: H01F 1/113 20060101ALI20191202BHEP

Ipc: B22F 8/00 20060101ALN20191202BHEP

Ipc: H01F 41/02 20060101AFI20191202BHEP

Ipc: B22F 7/08 20060101ALN20191202BHEP

INTG Intention to grant announced

Effective date: 20191216

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

Ref country code: AT

Ref legal event code: REF

Ref document number: 1277882

Country of ref document: AT

Kind code of ref document: T

Effective date: 20200615

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602018004998

Country of ref document: DE

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200904

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200603

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200903

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200603

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200603

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20200603

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200903

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200603

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200603

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200603

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 1277882

Country of ref document: AT

Kind code of ref document: T

Effective date: 20200603

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200603

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200603

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200603

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200603

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200603

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201006

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200603

Ref country code: IT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200603

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200603

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200603

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200603

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200603

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201003

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602018004998

Country of ref document: DE

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200603

26N No opposition filed

Effective date: 20210304

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200603

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200603

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20210426

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20210430

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20210430

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20210430

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20210426

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201003

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20210430

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20230309

Year of fee payment: 6

P01 Opt-out of the competence of the unified patent court (upc) registered

Effective date: 20230522

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200603

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20180426

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20230228

Year of fee payment: 6

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200603

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20240307

Year of fee payment: 7